EP 4160070 A1 20230405 - STRUCTURAL AND EQUIPMENT SYSTEM FOR INSTALLATION IN AN AIRCRAFT
Title (en)
STRUCTURAL AND EQUIPMENT SYSTEM FOR INSTALLATION IN AN AIRCRAFT
Title (de)
STRUKTUR- UND AUSSTATTUNGSSYSTEM ZUR INSTALLATION IN EINEM LUFTFAHRZEUG
Title (fr)
SYSTÈME STRUCTURAL ET D'ÉQUIPEMENT DESTINÉ À L'INSTALLATION DANS UN AÉRONEF
Publication
Application
Priority
EP 21200104 A 20210930
Abstract (en)
[origin: CN115892440A] The invention relates to a structure and equipment system for installation in an air vehicle, having a plurality of vertical supports, a guide rail arrangement, at least one connector, a plurality of guide elements, a plurality of pivot joints and a plurality of locking devices. The guide rail device is arranged on a structural part of the air vehicle for guiding a guide element along an extension axis of the guide rail device, the vertical supports are arranged parallel to one another by means of connecting pieces and are connected to form a grid structure on which the guide element is arranged, and the pivot joints can be mounted at the upper ends of the vertical supports, a locking device for pivoting the vertical support, the locking device having a first and a second locking element, by means of which guide elements on the guide rail device can be pushed into the structural part of the air vehicle with the vertical support pivoted upwards from the vertical direction towards the installation position, the first locking element can be locked into a correspondingly arranged second locking element by pivoting downward in a vertical orientation, whereby a load-bearing support structure can be formed.
Abstract (de)
Ein Struktur- und Ausstattungssystem (4) zur Installation in einem Luftfahrzeug, wobei eine Gitteranordnung (18) mittels Führungselemente (32) an einer Schienenvorrichtung (12) mit aus der Vertikalen aufwärts geschwenkten Vertikalstützen (14) in eine Struktur (6) des Luftfahrzeugs zu einer Installationsposition einschiebbar ist, durch Herabschwenken in eine vertikale Ausrichtung ersten Verriegelungselemente (22) in korrespondierend angeordneten zweiten Verriegelungselementen (20) verriegeln können, sodass dadurch eine lasttragende Stützstruktur ausbildbar ist.
IPC 8 full level
F16L 3/26 (2006.01); B64C 1/06 (2006.01); B64C 1/18 (2006.01); B64F 5/10 (2017.01); F16L 3/22 (2006.01); F16L 3/24 (2006.01); B65G 9/00 (2006.01); F16L 3/133 (2006.01)
CPC (source: EP US)
B64C 1/061 (2013.01 - EP US); B64C 1/18 (2013.01 - EP); B64C 1/20 (2013.01 - US); B64D 9/00 (2013.01 - US); B64F 5/10 (2017.01 - EP US); F16L 3/22 (2013.01 - EP); F16L 3/24 (2013.01 - EP); B64D 2009/006 (2013.01 - US); B64D 2221/00 (2013.01 - US); F16L 3/133 (2013.01 - EP)
Citation (applicant)
WO 2021122322 A1 20210624 - AIRBUS OPERATIONS GMBH [DE]
Citation (search report)
- [A] US 2021188417 A1 20210624 - MAUREL JEAN-LUC [FR], et al
- [A] EP 3838743 A1 20210623 - AIRBUS OPERATIONS SAS [FR]
- [A] US 2010031509 A1 20100211 - FRAUEN HOLGER [DE], et al
- [A] DE 102009056593 A1 20110609 - AIRBUS OPERATIONS GMBH [DE]
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
Designated extension state (EPC)
BA ME
Designated validation state (EPC)
KH MA MD TN
DOCDB simple family (publication)
EP 4160070 A1 20230405; CN 115892440 A 20230404; US 12006021 B2 20240611; US 2023105251 A1 20230406
DOCDB simple family (application)
EP 21200104 A 20210930; CN 202211128689 A 20220916; US 202217940067 A 20220908